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10.5 Moments of Inertia for
      Composite Areas
A composite area consist of a series of
connected simpler parts or shapes such as
semicircles, rectangles and triangles
Provided the moment of inertia of each of
these parts is known or can be determined
about a common axis, moment of inertia of
the composite area = algebraic sum of the
moments of inertia of all its parts
10.5 Moments of Inertia for
          Composite Areas
Procedure for Analysis
Composite Parts
  Using a sketch, divide the area into its composite
  parts and indicate the perpendicular distance
  from the centroid of each part to the reference
  axis

Parallel Axis Theorem
  Moment of inertia of each part is determined
  about its centroidal axis, which is parallel to the
  reference axis
10.5 Moments of Inertia for
          Composite Areas
Procedure for Analysis
Parallel Axis Theorem
  If the centroidal axis does not coincide with the
  reference axis, the parallel axis theorem is used
  to determine the moment of inertia of the part
  about the reference axis

Summation
  Moment of inertia of the entire area about the
  reference axis is determined by summing the
  results of its composite parts
10.5 Moments of Inertia for
         Composite Areas
Procedure for Analysis
Summation
  If the composite part has a hole, its moment
  of inertia is found by subtracting the moment
  of inertia of the hole from the moment of
  inertia of the entire part including the hole
10.5 Moments of Inertia for
            Composite Areas
Example 10.5
Compute the moment of
inertia of the composite
area about the x axis.
10.5 Moments of Inertia for
         Composite Areas
Solution
Composite Parts
  Composite area obtained
  by subtracting the circle
  form the rectangle
  Centroid of each area is
  located in the figure
10.5 Moments of Inertia for
         Composite Areas
Solution
Parallel Axis Theorem
  Circle
                               2
              I x = I x ' + Ad y
               1
               4
                               2    2
                                               ( )
              = π (25) + π (25) (75) = 11.4 106 mm 4
                      4



  Rectangle
                               2
              I x = I x ' + Ad y
                   1
              =
                  12
                                                         ( )
                     (100)(150)3 + (100)(150)(75)2 = 112.5 106 mm 4
10.5 Moments of Inertia for
         Composite Areas
Solution
Summation
  For moment of inertia for the composite
  area,
          I x = −11.4(106 ) + 112.5(10 6 )
                ( )
           = 101 10 6 mm 4
10.5 Moments of Inertia for
            Composite Areas
Example 10.6
Determine the moments
of inertia of the beam’s
cross-sectional area
about the x and y
centroidal axes.
10.5 Moments of Inertia for
            Composite Areas
Solution
Composite Parts
  Considered as 3
  composite areas A, B, and
  D
  Centroid of each area is
  located in the figure
10.5 Moments of Inertia for
         Composite Areas
Solution
Parallel Axis Theorem
  Rectangle A
                      2
     I x = I x ' + Ad y
         1
     =
        12
                                                  ( )
           (100)(300)3 + (100)(300)(200)2 = 1.425 109 mm 4
                      2
     I y = I y ' + Ad x
          1
     =
         12
                                                ( )
            (300)(100)3 + (100)(300)(250)2 = 1.90 109 mm 4
10.5 Moments of Inertia for
         Composite Areas
Solution
Parallel Axis Theorem
  Rectangle B
                         2
        I x = I x ' + Ad y
            1
        =
           12
                                 ( )
              (600)(100)3 = 0.05 109 mm 4
        I y = I y ' + Ad x2
             1
        =
            12
                                ( )
               (100)(600)3 = 1.80 109 mm 4
10.5 Moments of Inertia for
         Composite Areas
Solution
Parallel Axis Theorem
  Rectangle D
                     2
    I x = I x ' + Ad y
        1
    =
       12
                                                 ( )
          (100)(300)3 + (100)(300)(200)2 = 1.425 109 mm 4
                     2
    I y = I y ' + Ad x
         1
    =
        12
                                               ( )
           (300)(100)3 + (100)(300)(250)2 = 1.90 109 mm 4
10.5 Moments of Inertia for
         Composite Areas
Solution
Summation
  For moment of inertia for the entire cross-
  sectional area,
                ( )         ( )          ( )
      I x = 1.425 109 + 0.05 109 + 1.425 109
      = 2.90(10 )mm
               9       4


      I = 1.90(10 ) + 1.80(10 ) + 1.90(10 )
       y
                   9         9          9


      = 5.60(10 )mm
               9       4

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6161103 10.5 moments of inertia for composite areas

  • 1. 10.5 Moments of Inertia for Composite Areas A composite area consist of a series of connected simpler parts or shapes such as semicircles, rectangles and triangles Provided the moment of inertia of each of these parts is known or can be determined about a common axis, moment of inertia of the composite area = algebraic sum of the moments of inertia of all its parts
  • 2. 10.5 Moments of Inertia for Composite Areas Procedure for Analysis Composite Parts Using a sketch, divide the area into its composite parts and indicate the perpendicular distance from the centroid of each part to the reference axis Parallel Axis Theorem Moment of inertia of each part is determined about its centroidal axis, which is parallel to the reference axis
  • 3. 10.5 Moments of Inertia for Composite Areas Procedure for Analysis Parallel Axis Theorem If the centroidal axis does not coincide with the reference axis, the parallel axis theorem is used to determine the moment of inertia of the part about the reference axis Summation Moment of inertia of the entire area about the reference axis is determined by summing the results of its composite parts
  • 4. 10.5 Moments of Inertia for Composite Areas Procedure for Analysis Summation If the composite part has a hole, its moment of inertia is found by subtracting the moment of inertia of the hole from the moment of inertia of the entire part including the hole
  • 5. 10.5 Moments of Inertia for Composite Areas Example 10.5 Compute the moment of inertia of the composite area about the x axis.
  • 6. 10.5 Moments of Inertia for Composite Areas Solution Composite Parts Composite area obtained by subtracting the circle form the rectangle Centroid of each area is located in the figure
  • 7. 10.5 Moments of Inertia for Composite Areas Solution Parallel Axis Theorem Circle 2 I x = I x ' + Ad y 1 4 2 2 ( ) = π (25) + π (25) (75) = 11.4 106 mm 4 4 Rectangle 2 I x = I x ' + Ad y 1 = 12 ( ) (100)(150)3 + (100)(150)(75)2 = 112.5 106 mm 4
  • 8. 10.5 Moments of Inertia for Composite Areas Solution Summation For moment of inertia for the composite area, I x = −11.4(106 ) + 112.5(10 6 ) ( ) = 101 10 6 mm 4
  • 9. 10.5 Moments of Inertia for Composite Areas Example 10.6 Determine the moments of inertia of the beam’s cross-sectional area about the x and y centroidal axes.
  • 10. 10.5 Moments of Inertia for Composite Areas Solution Composite Parts Considered as 3 composite areas A, B, and D Centroid of each area is located in the figure
  • 11. 10.5 Moments of Inertia for Composite Areas Solution Parallel Axis Theorem Rectangle A 2 I x = I x ' + Ad y 1 = 12 ( ) (100)(300)3 + (100)(300)(200)2 = 1.425 109 mm 4 2 I y = I y ' + Ad x 1 = 12 ( ) (300)(100)3 + (100)(300)(250)2 = 1.90 109 mm 4
  • 12. 10.5 Moments of Inertia for Composite Areas Solution Parallel Axis Theorem Rectangle B 2 I x = I x ' + Ad y 1 = 12 ( ) (600)(100)3 = 0.05 109 mm 4 I y = I y ' + Ad x2 1 = 12 ( ) (100)(600)3 = 1.80 109 mm 4
  • 13. 10.5 Moments of Inertia for Composite Areas Solution Parallel Axis Theorem Rectangle D 2 I x = I x ' + Ad y 1 = 12 ( ) (100)(300)3 + (100)(300)(200)2 = 1.425 109 mm 4 2 I y = I y ' + Ad x 1 = 12 ( ) (300)(100)3 + (100)(300)(250)2 = 1.90 109 mm 4
  • 14. 10.5 Moments of Inertia for Composite Areas Solution Summation For moment of inertia for the entire cross- sectional area, ( ) ( ) ( ) I x = 1.425 109 + 0.05 109 + 1.425 109 = 2.90(10 )mm 9 4 I = 1.90(10 ) + 1.80(10 ) + 1.90(10 ) y 9 9 9 = 5.60(10 )mm 9 4